Transferring Structural Loads and Displacements Between Analysis and Design Software

ABSTRACT

Methods and apparatus, including computer program products, for receiving in a Computer Aided Design (CAD) tool result information and load information from a first analysis program, the result information determined by performing an analysis of a plurality of physical elements in a CAD model. And providing one or more of the result information or the load information from the CAD tool to a second analysis program.

BACKGROUND

Computer aided design (CAD) software is often used to prepare a CADmodel or models representing a structure, such as a building. The CADmodel can incorporate representations of physical elements, such ascolumns, beams, and the like that will be included in the structure.Drawings prepared from such a CAD model can be used in the actualphysical construction of the corresponding structure. The CAD model maybe prepared and edited by various individuals, including architects andstructural engineers.

As part of a design stage or after a design is completed, a structuralanalysis is typically performed on a structure. Structural analysis caninclude the computation of deformations, deflections, or internal forceson and within solid and non-solid structures based on information suchas a structure's geometry, applied loads and material properties ofphysical elements making up the structure. Result informationincorporates results from performing the structural analysis and canincorporate, for example, displacements, axial forces, bending moments,shear forces, stresses, load reaction information, and otherinformation. Result information can also incorporate a history of resultinformation over time.

Load information incorporates a representation of one or more appliedloads. An applied load is a force or forces applied to a component of astructure or to the structure as a whole. There are different types ofapplied loads. Commonly used applied loads can include constant loadsknown as dead loads (e.g., the weight of equipment, materials), staticloads known as live loads which typically represent a one time maximumvarying load on a structure (e.g., the weight of occupancy, automobileor foot traffic), loads proportional to exposed surface areas known asenvironmental loads (e.g., snow load, wind load, rain load), and dynamicloads. Dynamic loads typically involve dynamic effects such as fromwaves, ice flow, wind gusts, and earthquake motion. An applied load canbe represented as a combination of different load types. Moreover, loadinformation can represent a history of applied loads over time, such asmight be caused by applying an earthquake ground motion to thefoundation of a building.

Conventional analysis programs, tools, plugins or other suitableprocesses (hereinafter “programs”) receive as input by way of import oruser creation an analytical representation of a structure and,optionally, load information. Load information can be provided to ananalysis program and/or derived by the analysis program. For example,often material dead loads—such as the weight of beams and columns, areautomatically calculated by the analysis program, while environmentalloads are input by the user. An analytical representation of a structureis different than a representation of the physical elements, e.g.,columns, beams, etc. It is an idealized mathematical model that mayrepresent only a portion of a building such as one wing or one floor orone frame of the building. For example, an analytical representation maybe a wire frame representation of the physical elements, and the wireframe elements can include or have associated properties (e.g., weight,materials, moment of inertia, cross-sectional area), member connectivityand/or end conditions (e.g., pinned, free, fixed). Typically, theanalytical representation is prepared separately and can be used forother types of analyses that are performed in the design stage.

The analytical representation can be subjected to applied loadsimulation and the like in an analysis program to identify, for example,stress levels in the various elements. See, e.g., FIGS. 12-16. On thebasis of the analysis, elements may be modified (e.g., resized or otherproperties changed) and the modified analytical representationreanalyzed. A commonly used approach to performing structural analysisis the finite element approach which is a numerical method that models astructure as a discrete system with a finite number of elementsinterconnected at a finite number of nodes.

Depending on the structure and type of analyses required, multipleanalysis programs commonly need to be used. For example, specialfoundation analysis programs may be used to analyze different foundationconfigurations or variations in soil properties. Additionally, there areother programs used to analyze specialized structures such as billboardsor towers that are located on the tops of buildings. Results from oneanalysis are often iteratively used in another analysis. For example,the combination of wind and dead loads on a building can propagatethrough a structure and produce resultant loads on the foundation. Thoseloads may be used as input to a foundation analysis program. The resultsof the foundation analysis may have the consequence of changing thedesign (or the analytical model of the design), and the cycle ofbuilding and foundation analyses is commenced again.

Any change to the size or location (i.e., displacement) of physicalmembers or their applied loading typically needs to be manually updatedbetween the multiple analysis and design programs. For example,foundation reactions from a seismic analysis of the structure arecommonly transcribed and used as input for a foundation analysisprogram. The effort and coordination involved with synchronizing thesedisplacements and loadings between programs can be significant. Anyout-of-synch issues could result in an inadequate design being taken toconstruction.

SUMMARY

This specification describes systems, techniques and computer programsfor transferring load and result information between structural analysisand design programs.

In one general aspect, the techniques feature receiving in a CAD toolresult information and load information from a first analysis program,the result information determined by performing an analysis of aplurality of physical elements in a CAD model. One or more of the resultinformation or the load information is provided from the CAD tool to asecond analysis program.

The invention can be implemented to include one or more of the followingadvantageous features. The CAD model is associated with the CAD tool.Incorporating one or more of the result information or the loadinformation into the CAD model. The first analysis program or the secondanalysis program can be invoked. The load information incorporates arepresentation of one or more applied loads. The load informationincorporates a history of applied loads over time. The resultinformation incorporates one or more of: a displacements, an axialforce, a bending moment, a shear force, a stress, or load reactioninformation. The result information incorporates a history of resultsover time.

In another general aspect, the techniques feature receiving in a CADtool one or more displacements from a first analysis program, the one ormore displacements based on performing an analysis of a plurality ofphysical elements in a CAD model, including applying one or more loadsto the plurality of physical elements. One or more of the one or moredisplacements or one or more loads from the CAD tool is provided to asecond analysis program.

The invention can be implemented to include one or more of the followingadvantageous features. The CAD model is associated with the CAD tool.The one or more displacements and the one or more loads are incorporatedinto the CAD model. One or more of: the first analysis program or thesecond analysis program are invoked. The one or more loads incorporatesa history of applied loads over time. The one or more displacementsincorporates a history of displacements over time.

Implementations of the invention can realize one or more of thefollowing advantages. A physical representation, a correspondinganalytical representation, load information, and result information canbe integrated in a single CAD model. Each analysis program can useinformation in the CAD model, modify information in the CAD model, andadd information to the CAD model. Results from an analysis by oneanalysis program can be easily provided to other analysis programs. Loadand result information can be maintained and coordinated betweenmultiple analysis and design programs. Various structural analysisprograms can be used, and other types of analysis can be performed,including concrete design analysis, lateral load analysis, gravity loadanalysis, beam design analysis, steel design analysis, dynamic analysis,seismic analysis and steel connection design analysis.

The details of one or more implementations of the invention are setforth in the accompanying drawings and the description below. Otherfeatures, aspects, and advantages of the invention will be apparent fromthe description and drawings, and from the claims.

DESCRIPTION OF DRAWINGS

FIG. 1 shows a user interface for viewing and manipulating one or morecomputer aided design models.

FIG. 2 shows a user interface displaying two views of a CAD model.

FIG. 3 shows a user interface displaying two views of a CAD model.

FIG. 4 shows a user interface displaying an elevation view combiningphysical and analytical representations.

FIG. 5 shows a user interface displaying a plan view combining physicaland analytical representations.

FIG. 6 shows a user interface displaying a plan view combining physicaland analytical representations and illustrating a divergence therebetween.

FIG. 7 shows a user interface displaying a 3D view combining physicaland analytical representations of a CAD model.

FIG. 8 shows a user interface displaying a 3D view combining physicaland analytical representations of a CAD model.

FIG. 9 is a schematic representation illustrating an override as adefault analytical representation.

FIG. 10 shows a user interface for exchanging information betweenanalysis programs.

FIG. 11 is an example of an analysis program user interface.

FIGS. 12-16 illustrate how external loads can be propagated through astructure by an analysis program.

FIG. 17 is a detailed system diagram of a CAD tool.

FIG. 18 is a flow diagram illustrating transference of informationbetween analysis programs and a CAD tool.

FIG. 19 is a flow diagram illustrating transference of informationbetween analysis programs and a CAD tool.

FIG. 20 is a further flow diagram illustrating transference ofinformation between analysis programs and a CAD tool.

Like reference symbols in the various drawings indicate like elements.

DETAILED DESCRIPTION

FIG. 1 shows a user interface 100 for viewing and manipulating one ormore CAD models. The user interface 100 can be presented by aninteractive CAD program or tool that allows for the viewing, creating,and modifying of one or more CAD models. In one implementation, the CADtool is Autodesk® Revit® Structure, available from Autodesk, Inc. of SanRafael, Calif. Generally speaking, a CAD model is one or more CADmodels, or a view of one or more CAD models, or combinations of these. ACAD model can contain information required to represent one or morephysical and analytical elements, and relationships between them, loadinformation, and result information. For example, a CAD model can storeone or more representations of a CAD model of a building. A CAD modelcan be stored in one or more files, object-oriented databases,relational databases, distributed objects, caches, data structures,combinations of these, or other suitable storage. The term “model” asused herein is synonymous with the CAD model's contents.

Although a graphical user interface (GUI) is illustrated, other userinterfaces are possible, including user interfaces that allow for userinteraction by means of sound, voice, gesture, eye movement, use ofremote control devices, manually controlled devices, and combinations ofthese. The user interface can be provided on a number of computingdevices including, but not limited to, devices such as a workstations,personal computers, cellular telephones, personal digital assistants,portable video playback devices, combinations of these, and othersuitable devices. In one implementation, the user interface can bepresented as one or more web pages. By way of illustration, the CAD toolcan execute on one or more computing devices connected by one or morewired or wireless networks, shared memory, inter-processor networks, orother suitable means. A computing device can run a proprietary orcommercially available multi-tasking operating system such as, withoutlimitation, Microsoft Windows® XP (available from Microsoft Corp. ofRedmond, Wash.), Linux (available from www.lixuxlinux.org), and Apple OSX (available from Apple Computer, Inc. of Cupertino, Calif.).

The user interface 100 illustrated in FIG. 1 can present one or moreviews of one or more models. A three dimensional (3D) view 102 presentsa physical representation of a CAD model of a building. The view 102 canbe used to create and modify the physical representation 104. Thephysical representation 104 depicts physical elements of the buildingrepresented by the CAD model including, without limitation, beams,braces, floors, slabs, columns, walls, and isolated and continuousfootings. In one implementation and by way of illustration, the userinterface 100 includes a view panel 108, which allows a user to selectviews and display one or multiple views in the user interface 100. Theview panel 108 includes, but is not limited to, two dimensional (2D) and3D views, plans, elevations, sectional views, analytical views, andcombinations of these. View 102 shows a CAD model of a building section106 having beams 114 and 118, and footings 110 and 112. Physicalelements can be associated with attributes. In one implementation,physical element attributes include, without limitation, geometry,location, weight, cross sectional area, construction materials,reference to one or more corresponding analytical elements, and othersuitable properties. Attribute values can be specified by the user orprovided by default.

FIG. 2 illustrates additional views of the CAD model representing abuilding. A 3D view 204 showing an analytical representation 205 ofsection 106 is presented. The view 204 can be used to view and modifythe analytical representation 205. The analytical representation 205depicts analytical elements corresponding to the physical elementsincluded in the physical representation 104. In one implementation, agiven physical element may not have a corresponding analytical element.The analytical representation 205 can be generated automatically as theuser creates or modifies physical elements. In one implementation,analytical elements are simplified versions of physical elements. Forexample, an analytical element can be a line or a planar surface. SeeTable 1. In a further implementation, an association between a givenphysical element in the physical representation 104 and one or morecorresponding analytical elements in the analytical representation 205can be established by, for example, including a reference to the one ormore analytical elements in the physical element's attributes.

In one implementation, the analytical elements are automaticallyconnected to one another to form a wire frame representation of the CADmodel. In one implementation, a predetermined type of analytical elementcorresponds to a particular type or types of physical elements. Thus,when generating an analytical representation corresponding to thephysical representation, analytical elements corresponding to physicalelements can be created accordingly. In one implementation, ananalytical element has a default position in relation to the analyticalelement's corresponding physical element(s). See Table 1. For example, aphysical element representing a column has a corresponding analyticalelement that is a line that runs through the center of the columnlocation.

TABLE 1 PHYSICAL ANALYTICAL DEFAULT LOCATION OF ELEMENT ELEMENTANALYTICAL ELEMENT Beam Line Parallel and centered on the top surface ofthe beam for floors and centered for trusses. Brace Line Parallelthrough the center of the brace. Column Line Parallel through the centerof the column. Wall Planar Surface Parallel through the center plane ofthe wall. Floor/Slab Planar Surface Parallel on the top surface offloor/slab or in the mid plane of the floor/slab.

As the analytical representation is generated in parallel with thephysical representation, connections between physical elements causeconnections to be made between analytical elements. In some instances,the location of an analytical element is deviated from the defaultlocation so that that the analytical element may connect to anotheranalytical element. As a result, an analytical element may be partiallycoincident with, or incongruous to, a corresponding physical element. Inone implementation, connections between analytical elements maintaincoherence in the analytical representation. Coherence takes into accountthe probable location of finite element analysis nodes on analyticalelements (e.g., for structural analysis) and guides connections betweenanalytical elements to these locations. A node is a point at whichdifferent elements are joined together and where values of unknowns canbe approximated. By way of illustration, if the analyticalrepresentation of a physical element representing a beam is attached atone end to the surface of a physical element representing a column, thecorresponding analytical element representing the beam (which is a linecentered on the top surface of the physical element representing thebeam) will pass through the physical element representing the column toconnect with the analytical element representing the column (which is aline located at the center of the column).

Default analytical element locations and coherence requirements can bedescribed by rules or information which can be created and modified bythe user or by an analysis program. In one implementation, coherence ofthe analytical representation is not a prerequisite to performingstructural analysis of the CAD model. In one implementation, the defaultlocation and connectivity of an analytical element can be overridden bythe user.

The analytical representation can include, without limitation, thefollowing attributes: geometry, location, moments of inertia, sheercapacity, connectivity or end conditions (e.g., pinned, fixed, free),material properties, reference to one or more corresponding physicalelements, and release conditions. Attribute values can be specified by auser or provided by default. In one implementation, default attributevalues can be determined based on heuristics informed by, for exampleand without limitation, the user's past interaction with the CAD model,the materials and geometries of the physical elements, building codes,historical weather patterns for a given location, and the purpose of thestructure (e.g., office, hospital, school, condominium, parking garage,etc.).

When an attribute of an analytical element is modified, thecorresponding physical element can be adjusted to reflect themodification. In one implementation, when an analytical elementattribute is changed, analytical elements that are connected to theanalytical element are adjusted, if necessary to maintain coherency. Forinstance, if the user moved the location of an analytical elementrepresenting a horizontal beam, then analytical elements connected tothe moved analytical element would be moved or resized accordingly, inorder to maintain their coherent connection to the beam. In oneimplementation, changing the location or size of an analytical elementdoes not change the location of the analytical element's correspondingphysical element.

Referring again to FIG. 2, the analytical view 204 includes analyticalelements representing columns (114′, 118′) and a beam 206′ connectingthe columns (114′, 118′). A 2D elevation view 202 of the physicalrepresentation of the section 106 shows the corresponding physicalelements 114, 118 and 206. Changes made to physical element attributescan be automatically reflected in corresponding analytical elements, andvice versa. In one implementation, changing the location of ananalytical element does not cause the corresponding physical element tochange its location. This allows a user to manipulate the analyticalrepresentation to capture eccentricities such as a torque or turning notmanifest in the physical representation.

FIG. 3 shows the section 106 shown in FIG. 2 after a physical element300 representing a support brace has been added. In this illustration,addition of the physical element 300 (as shown in view 202)automatically causes the generation of a corresponding analyticalelement 300′ shown in view 204. The analytical representation isautomatically maintained as the user creates, modifies, or deletesphysical elements. For example, if the user moves or deletes thephysical element 300, the counterpart element 300′ is automaticallymoved or deleted. In one implementation and by way of furtherillustration, if the user moves or deletes the analytical element 300′,the counterpart physical element 300 is not moved or deleted. (In oneimplementation the user can manipulate the analytical representation anddefeat coherence.) As illustrated in FIG. 4, the default location of theanalytical element 300′ is not required to be entirely coincident withthe physical element 300, in order to achieve coherence in theanalytical representation.

FIG. 4 shows an elevation view 400 that combines physical and analyticalrepresentations. In this illustration, a physical element 406representing a brace 406 has been added to section 106. Each physicalelement (206, 300, 406, 114) has a corresponding analytical element(206′, 300′, 406′, 114′) that was automatically generated. Notice thatthe analytical element 114′ representing a column is parallel to andcoincident with the center of the physical element 114 representing thecolumn. The analytical element 206′ representing the beam is coincidentwith the top surface of the physical beam 206. In one implementation,analytical elements representing physical beams, floors and slabs arecoincident with the top surfaces of the corresponding physical elementsbased on the assumption that top surfaces are where finite elementanalysis nodes are located for structural analysis purposes. Noticehowever that the analytical elements 300′ and 406′ representing bracesare not coincident with the top surfaces of the corresponding physicalelements 300 and 406. In one implementation, coherence requires theanalytical elements connect with the analytical element 206′representing the beam at the center point 402 of the analytical element206′ representing the beam. This would not be the case if the analyticalelements 300′ and 406′ representing the cross beams were entirelycoincident with their corresponding physical elements. In oneimplementation the user can manipulate the analytical representation anddefeat coherence.

FIG. 5 shows a plan view 500 that combines physical and analyticalrepresentations. The physical element 504 representing a column has acorresponding analytical element 504′, which is represented by thecenter point of the element 504 representing the column. In an elevationview of the element 504 representing the column, the analytical element504′ representing the column would appear as a vertical line runningthrough the center of the column. Physical elements 506, 510, 512 and516 representing beams all abut the physical element 504 representingthe column. However, the analytical elements 506′, 510′, 512′ and 516′representing the beams extend into the physical element 504 representingthe column to connect with the analytical element 504′ representing thecolumn in order to create a coherent representation. The element 508 isa secondary beam supported by the two primary beams 510 and 506. Theanalytical element 508′ representing the secondary beam lies on the topsurface of the physical element 508 representing the secondary beam andconnects to analytical elements 510′ and 506′ representing the primarybeams at either end. Likewise, element 514 representing the secondarybeam supported by the two primary beams 512 and 516. The analyticalelement 514′ representing the secondary beam lies on the top surface ofthe physical element 514 and connects to analytical elements 512′ and516′ representing the primary beams at either end. The physical element510 representing a beam abuts physical element 502 representing a wall.The analytical element 510′ representing the beam connects to theanalytical element '502 representing the wall plane which lies in thecenter of the element 502 representing the wall.

FIG. 6 illustrates divergence of an analytical representation from aphysical representation. As presented in view 500, physical elements 516and 510 representing the beams have been moved to place them off centerfrom physical element 504 representing the column. Notice, however, thatthe corresponding analytical elements 510′ and 516′ have by defaultremained connected to the analytical element 504′ representing thecolumn even though the analytical elements 510′ and 516′ are no longercoincident with their corresponding physical elements 510 and 516representing the beams. This is to preserve the coherence of theanalytical representation. However, as discussed above, the user canoverride the default configuration of the analytical representation.

FIG. 7 shows a 3D view that combines physical and analyticalrepresentations of two walls. Physical element 510 representing a beamabuts physical element 502 representing a lower wall while thecorresponding analytical element 510′ representing the beam connects tothe analytical element 604′ corresponding to a physical element 604representing the beam on the other side of the physical element 502representing the wall. Physical element 602 representing an upper wallis supported by physical element 502 representing the lower wall.Although the surfaces of the elements 502 and 602 representing the wallslie in the same plane on one side, the surfaces on the other side do notsince the element 502 representing the lower wall is thicker than theelement 602 representing the upper wall. The analytical model for walls502 and 602 is a surface and the default location is the center plane ofthe wall. The analytical elements for the element 602 representing theupper wall and the element 502 representing the lower wall do not lie inthe same plane. From a structural analysis standpoint, this means thatthe upper wall is not supported by the lower wall. In oneimplementation, one of the upper 602′ or lower 502′ analytical wallelements is automatically moved to be in line with the other. In otherimplementation, the user can manually move one or both of the analyticalelements 602′ and 502′ so they lie in the same plane. The decision canbe based on engineering judgment. View 600 in FIG. 8 shows theanalytical wall elements 602′ and 502′ in alignment as a result ofmoving the analytical wall element 502′. Notice how the physical wallelements 502 did not change location.

FIG. 9 presents another example of overriding the default analyticalrepresentation. In part (a) of FIG. 9, a wall consisting of fivephysical wall elements (902, 904, 906, 908, 910) is shown along with thewall's corresponding default analytical representation consisting ofanalytical wall elements (902′, 904′, 906′, 908′, 910′). In part (b) ofFIG. 9, a user has decided not to have an analytical model for wallelements 904′ and 908′, and projected analytical wall element '906 to bein alignment with elements '902 and '910.

In one implementation, structural analysis of a CAD model (or portionsthereof) can be initiated from the CAD tool, as shown in FIG. 10. Userscan select an analysis program to invoke, for example, by selecting the“Tools/External Tools” 1000 menu item in the user interface 100, andthen selecting the “Send Model to . . . ” menu item 1002. This selectioncauses a list identifying one or more analysis programs to be presentedfrom which the user can chose a desired program. This analysis programis then invoked (if it is not already running) and CAD model information(e.g., a physical representation, an analytical representation, andanalytical information) is transferred to the analysis program. Theanalysis program can optionally present its own user interface (e.g.,1100 in FIG. 11) in combination with the user interface 100 or byitself.

In one implementation, after the analysis program has completed itsfunction, or while it is performing its function, the analysis programcan then update the CAD model with changes to element properties andanalysis information (i.e., load information and/or result information).This integrated model capability allows analysis programs to shareinformation and build on the results of earlier invoked analysisprograms.

Users have the option of selecting a number of physical or analyticalelements before invoking an analysis program. In which case, the programcan either perform its analysis on the selected elements or give usersthe option to perform analysis on the full model. An analysis programcan also provide users with the ability to select which element typesare to be analyzed.

The analysis program can optionally prompt users to provide additionalinput that is not available in the transferred CAD model information,such as by presenting a dialog box whereby a user can specify theinformation or the information's location. Users can optionally alsoselect which elements whose properties are modified by the analysisprogram are to be automatically updated in the CAD model. For example,the analysis program might change the thickness and position of columnsin a physical representation.

In another implementation, the analysis program does not have to persistits results in the CAD model. Instead, an analysis program might storeresults in its own database or CAD model. Users can import suchinformation into the CAD model using the “Update Model from . . . ” menuitem 1204.

FIGS. 12-16 illustrate how external loads can be propagated through astructure by an analysis program. FIG. 12 is an elevation view 1200 of abuilding where an external distributed load that represents live loadsis applied, as depicted by the downward pointing arrows 1202.

FIG. 13 shows the external load 1202 being distributed by the analysisprogram to create three load reactions: 1302, 1304 and 1306. Themagnitude of the reactions is different based on the span length and thestiffness of beams and columns. These reactions become loads applied onthe supporting columns 1308, 1310 and 1312, respectively.

FIG. 14 illustrates that the load reactions 1302, 1304 and 1306 havebeen transferred by the columns 1308, 1310 and 1312 to membersunderneath, which are the columns on the left 1402, the right 1406 and abeam 1404 in the center.

FIG. 15 illustrates left and right load reactions (1302 and 1306)propagating directly down to the foundations 1502 and 1504,respectively.

Finally, FIG. 16. illustrates the central load reaction 1304 beingdistributed again between the columns 1402, 1602 and 1406 that supportthe beam 1404. The load reactions 1304 will propagate to the foundationas before and the analysis program can accumulate all of the loads thatare applied to any member so that for the foundations 1502, 1504 and1506 a total load can be the sum of the distribution of all thereactions in the structure.

Load information and/or result information that are determined by theanalysis program can be provided to the CAD tool. By way ofillustration, if a user wants to design a foundation (e.g., calculatethe size of the foundation and the reinforcement inside), the user canuse another analysis program, perhaps from a different softwarepublisher, that will extract the foundation information and loadreactions calculated by the first analysis program. The user does nothave to manually transfer the output of the first analysis program tothe second analysis program. This is done automatically. As such, timeis saved and errors that could result from manual manipulation of thedata are avoided.

FIG. 17 is a system diagram of CAD tool 1700 and various analysisprograms 1704, 1708, and 1710. In one implementation, commerciallyavailable analysis programs can be used to perform the analysis. Theanalysis programs 1704, 1708, and 1710 can be tightly integrated withthe CAD tool 1700 (e.g., as a plug-in module or dynamic link library) orloosely integrated (e.g., requiring export of the CAD model informationto another process or persistent storage). As examples, the followingcommercially available analysis programs can be used: ETABS, availablefrom Computers and Structures, Inc. of Berkeley, Calif.; RISA-3D,available from RISA Technologies of Foothill Ranch, Calif.; or ROBOTMillennium available from RoboBAT/ISS Inc. Other types of analysisprograms can be integrated with the CAD tool 1700 including, but notlimited to, concrete design analysis, lateral load analysis, gravityload analysis, beam design analysis, steel design analysis, dynamicanalysis, seismic analysis and steel connection design analysis.

When the user invokes an analysis program 1704, 1708, or 1710 from theCAD tool 1700, the CAD tool 1700 can transfer CAD model 1702 informationto the selected analysis program by way of a transfer engine 1712.Alternatively, the analysis program can access the CAD model 1702 itselfby way of transfer engine 1712 and obtain the information needed toperform the analysis. As analysis is being performed, or duringanalysis, analysis results are transferred to the CAD model by way oftransfer engine 1712 as initiated by the invoked analysis program or bythe CAD tool 1700. In one implementation, transfer engine 1712 is aprogramming interface or protocol incorporating functionality fortransferring information between the CAD tool 1700 and one or multipleanalysis programs. The analysis programs and the CAD tool can execute onthe same computing device, or on different computing devices connectedby one or more shared or private computer networks, shared memory,combinations of these, or other suitable means.

An analysis program can maintain a concurrent database 1706 which can beused to store information that users can add or modify inside theanalysis application. In one implementation, every element in the CADmodel 1702 has a unique element identifier (ID). This ID can be used bythe analysis program to correlate data in the CAD model 1702 with datain the database 1706. A synchronization process may be required toinsure that when the analysis application is invoked that data in thedatabase 1706 accurately reflects the data in the CAD model 1702. Forexample the user may have added, removed or changed elements in the CADmodel 1702.

FIG. 18 shows a system 1800 for exchanging information between one ormore analysis programs (1704, 1708, 1710) with the CAD model 1702. Theuser interface 100 provides one or more views (1804, 1806, 1808) of theCAD model 1702. Generally speaking, a view (1804, 1806, 1808) canpresent n-dimensions (e.g., 2D, 3D) of information pertaining to the CADmodel 1702. Views can, for example, be scaled, rotated and translated. Aview can optionally present an altered version of the CAD model byapplying one or more filters (1814, 1816, 1818) to the CAD model 1702. Afilter can screen out certain types of information that are of nointerest to a given view. For example, a physical view can use a filterto screen out analytical representations of physical elements, whereas apurely analytical view can use a filter to screen out physical elements.Alternatively, a filter can interact with elements in the CAD model 1702in order to obtain specific representations of the element. For example,an element could render itself as a solid, physical object, as ananalytical representation of the physical object, or both.

In one implementation, the user interface 100 propagates informationpertaining to changes the user makes to the CAD model 1702 through oneor more views (1804, 1806, 1808) to a change engine 1810. The changeengine 1810 accepts this information and uses it to maintainsynchronization between the analytical representation and the physicalrepresentation of the CAD model 1702. For example, if a user moves aphysical element, the change engine 1810 moves the correspondinganalytical element(s) (as necessary) to maintain coherence in theanalytical representation. Likewise, changes to attributes made in onerepresentation are reflected in the other by the change engine 1810. Thechange engine 1810 generates the analytical representation as the userinteractively generates or edits the physical representation.

Analysis of a physical or analytical representation in the CAD model1702 can be initiated by the analysis component 1812. In oneimplementation, the analysis component 1812 invokes one or more analysisprograms (1704, 1708, 1710) as a result of selection of menu item 1002in user interface 100, for example. An analysis program can be invokedthrough an application programming interface (API) 1820. The API 1820communicates with an analysis program (1704, 1708, 1710) through aservice provider interface (SPI), such as 1822, 1824 and 1826. In oneimplementation, each analysis program (1704, 1708, 1710) implements theSPI. The API 1820 and the SPIs (1822, 1824, 1826) can implement acommunication protocol that exchanges information using memory buffers,shared memory, dynamically linked libraries, network communicationmechanisms, or other suitable means including more than one of these.

In one implementation, an API and an SPI are instantiations of objects.An API object's methods invoke an SPI object's methods (or vice versa)in order to transfer model information and perform analysis. Forexample, an analysis program may need to obtain CAD model 1702information or otherwise convert CAD model 1702 information into aformat suitable for analysis. In a further implementation, the API 1820can cause an analysis program to present a GUI through which the usercan monitor and control the analysis. In another implementation, ananalysis program can read and write information to the CAD model 1702(e.g., through an SPI or other suitable means).

The analysis program, or the user of the analysis program, can changeattributes of both physical and analytical elements in the CAD model1702. For example, the size of elements can be increased to accommodateloads. In one implementation, physical and analytical element attributescan be recognized by the structural analysis programs (1704, 1708,1710). These changes to element attributes and/or analysis informationare, in one implementation, automatically incorporated into the CADmodel 1702 directly or indirectly (e.g., by importing information froman analysis program) thereby making the changes immediately availablefor viewing in the user interface 100. In this way, multiple analysisprograms can share information.

The system 1800 may have fewer or more components than those illustratedin FIG. 18. A given component can execute on one or more communicablycoupled computing devices. For instance, computing devices can beconnected by a wired network, a wireless network, the Internet, sharedmemory, an inter-processor communication channel, or combinations ofthese.

FIG. 19 is a flow diagram illustrating transference of informationbetween analysis programs and a CAD tool. A CAD tool (e.g., 1700)receives result information and load information from an analysisprogram (e.g., 1704, step 1902). In one implementation, the informationcan be transferred through use of an SPI (1822, 1824, 1826) from ananalysis program to the CAD tool 1700 and stored in the CAD model 1702.The result information can be determined by performing an analysis of aplurality of physical elements in a CAD model, for example and asdescribed above. One or more of the result information or the loadinformation from the CAD tool is provided to a second analysis program(e.g., 1708, step 1904). In one implementation, the information istransferred from the CAD model 1702 to the second analysis programthrough use of an SPI (1822, 1824, 1826).

FIG. 20 is further flow diagram illustrating transference of informationbetween analysis programs and a CAD tool. A CAD tool (e.g., 1700)receives one or more displacements from a first analysis program (e.g.,1704), the one or more displacements based on performing an analysis ofa plurality of physical elements in a CAD model (step 2002). In oneimplementation, the displacements can be transferred through use of anSPI (1822, 1824, 1826) from an analysis program to the CAD tool 1700 andstored in the CAD model 1702. One or more displacements and/or one ormore loads from the CAD tool are provided to a second analysis program(e.g., 1708, step 2004). In one implementation, the displacements and/orloads can be transferred from the CAD model 1702 to the second analysisprogram through use of an SPI (1822, 1824, 1826).

The invention and all of the functional operations described in thisspecification can be implemented in digital electronic circuitry, or incomputer software, firmware, or hardware, including the structural meansdisclosed in this specification and structural equivalents thereof, orin combinations of them. The invention can be implemented as one or morecomputer program products, i.e., one or more computer programs tangiblyembodied in an information carrier, e.g., in a machine readable storagedevice or in a propagated signal, for execution by, or to control theoperation of, data processing apparatus, e.g., a programmable processor,a computer, or multiple computers.

A computer program (also known as a program, software, softwareapplication, or code) can be written in any form of programminglanguage, including compiled or interpreted languages, and it can bedeployed in any form, including as a stand alone program or as a module,component, subroutine, or other unit suitable for use in a computingenvironment. A computer program does not necessarily correspond to afile. A program can be stored in a portion of a file that holds otherprograms or data, in a single file dedicated to the program in question,or in multiple coordinated files (e.g., files that store one or moremodules, sub programs, or portions of code). A computer program can bedeployed to be executed on one computer or on multiple computers at onesite or distributed across multiple sites and interconnected by acommunication network.

The processes and logic flows described in this specification, includingthe method steps of the invention, can be performed by one or moreprogrammable processors executing one or more computer programs toperform functions of the invention by operating on input data andgenerating output. The processes and logic flows can also be performedby, and apparatus of the invention can be implemented as, specialpurpose logic circuitry, e.g., an FPGA (field programmable gate array)or an ASIC (application specific integrated circuit).

Processors suitable for the execution of a computer program include, byway of example, both general and special purpose microprocessors, andany one or more processors of any kind of digital computer. Generally, aprocessor will receive instructions and data from a read only memory ora random access memory or both. The essential elements of a computer area processor for executing instructions and one or more memory devicesfor storing instructions and data. Generally, a computer will alsoinclude, or be operatively coupled to receive data from or transfer datato, or both, one or more mass storage devices for storing data, e.g.,magnetic, magneto optical disks, or optical disks. Information carrierssuitable for embodying computer program instructions and data includeall forms of non volatile memory, including by way of examplesemiconductor memory devices, e.g., EPROM, EEPROM, and flash memorydevices; magnetic disks, e.g., internal hard disks or removable disks;magneto optical disks; and CD ROM and DVD-ROM disks. The processor andthe memory can be supplemented by, or incorporated in, special purposelogic circuitry.

To provide for interaction with a user, the invention can be implementedon a computer having a display device, e.g., a CRT (cathode ray tube) orLCD (liquid crystal display) monitor, for displaying information to theuser and a keyboard and a pointing device, e.g., a mouse or a trackball,by which the user can provide input to the computer. Other kinds ofdevices can be used to provide for interaction with a user as well; forexample, feedback provided to the user can be any form of sensoryfeedback, e.g., visual feedback, auditory feedback, or tactile feedback;and input from the user can be received in any form, including acoustic,speech, or tactile input.

The invention can be implemented in a computing system that includes aback end component (e.g., a data server), a middleware component (e.g.,an application server), or a front end component (e.g., a clientcomputer having a graphical user interface or a Web browser throughwhich a user can interact with an implementation of the invention), orany combination of such back end, middleware, and front end components.The components of the system can be interconnected by any form or mediumof digital data communication, e.g., a communication network. Examplesof communication networks include a local area network (“LAN”) and awide area network (“WAN”), e.g., the Internet.

The computing system can include clients and servers. A client andserver are generally remote from each other and typically interactthrough a communication network. The relationship of client and serverarises by virtue of computer programs running on the respectivecomputers and having a client-server relationship to each other.

The invention has been described in terms of particular embodiments, butother embodiments can be implemented and are within the scope of thefollowing claims. For example, the operations of the invention can beperformed in a different order and still achieve desirable results. Incertain implementations, multitasking and parallel processing may bepreferable. Other embodiments are within the scope of the followingclaims

1-20. (canceled)
 21. A computer-implemented method, comprising: storinga representation of elements of a physical structure in a computer aideddesign (CAD) model; providing the representation of elements to a firstanalysis program for application of simulated loads to therepresentation of elements; storing in the CAD model first loadinformation that specifies the simulated loads applied by the firstanalysis program; providing the representation of elements to a secondanalysis program for application of simulated loads to therepresentation of elements; and storing in the CAD model second loadinformation that specifies the simulated loads applied by the secondanalysis program so that the CAD model includes a history of loadsapplied by the first and second analysis programs.
 22. Thecomputer-implemented method of claim 21, further comprising: modifyingthe representation of elements based on result information thatidentifies changes to the representation of elements and that wasdetermined by the first analysis program's application of the simulatedloads to the representation of elements; and wherein the representationof elements that is provided to the second analysis program has beenmodified based on the result information.
 23. The computer-implementedmethod of claim 22, further comprising: receiving the result informationby a CAD tool application program and from the analysis program; andwherein the CAD tool performs the modifying of the representation ofelements.
 24. The computer-implemented method of claim 23: whereinproviding the representation of elements to the second analysis programincludes providing the first load information to the second analysisprogram; and further comprising extracting, by the second analysisprogram, the result information that identifies changes to therepresentation of elements from the CAD model using the first loadinformation provided to the second analysis program.
 25. Thecomputer-implemented method of claim 21, wherein providing therepresentation of elements to the second analysis program includesproviding the first load information to the second analysis program. 26.The computer-implemented method of claim 21, wherein providing therepresentation of elements to the second analysis program includesautomatically transferring the first load information to the secondanalysis program without receiving user input that manually transfers tothe second analysis program the simulated loads that were applied by thefirst analysis program.
 27. The computer-implemented method of claim 21,further comprising: receiving user input to create a physical element ina physical representation of elements that is stored in the CAD model;and in response to receiving the user input to create the physicalelement, generating the physical element in the physical representationof elements, and generating a corresponding analytical element in therepresentation of elements that is stored in the CAD model.
 28. Thecomputer-implemented method of claim 21, wherein the storing andproviding are performed by a CAD tool application program executing on acomputer system.
 29. A computer program product tangibly embodied in acomputer-readable storage device and comprising instructions that whenexecuted by a processor perform operations comprising: storing arepresentation of elements of a physical structure in a computer aideddesign (CAD) model; providing the representation of elements to a firstanalysis program for application of simulated loads to therepresentation of elements; storing in the CAD model first loadinformation that specifies the simulated loads applied by the firstanalysis program; providing the representation of elements to a secondanalysis program for application of simulated loads to therepresentation of elements; and storing in the CAD model second loadinformation that specifies the simulated loads applied by the secondanalysis program so that the CAD model includes a history of loadsapplied by the first and second analysis programs.
 30. The computerprogram product of claim 29, wherein the operations further comprise:modifying the representation of elements based on result informationthat identifies changes to the representation of elements and that wasdetermined by the first analysis program's application of the simulatedloads to the representation of elements; and wherein the representationof elements that is provided to the second analysis program has beenmodified based on the result information.
 31. The computer programproduct of claim 30, wherein the operations further comprise: receivingthe result information by a CAD tool application program and from theanalysis program; and wherein the CAD tool performs the modifying of therepresentation of elements.
 32. The computer program product of claim31: wherein providing the representation of elements to the secondanalysis program includes providing the first load information to thesecond analysis program; and wherein the operations further compriseextracting, by the second analysis program, the result information thatidentifies changes to the representation of elements from the CAD modelusing the first load information provided to the second analysisprogram.
 33. The computer program product of claim 29, wherein providingthe representation of elements to the second analysis program includesproviding the first load information to the second analysis program. 34.The computer program product of claim 29, wherein providing therepresentation of elements to the second analysis program includesautomatically transferring the first load information to the secondanalysis program without receiving user input that manually transfers tothe second analysis program the simulated loads that were applied by thefirst analysis program.
 35. The computer program product of claim 29,wherein the operations further comprise: receiving user input to createa physical element in a physical representation of elements that isstored in the CAD model; and in response to receiving the user input tocreate the physical element, generating the physical element in thephysical representation of elements, and generating a correspondinganalytical element in the representation of elements that is stored inthe CAD model.
 36. The computer program product of claim 29, wherein thestoring and providing are performed by a CAD tool application programexecuting on a computer system.
 37. A system comprising: a computerreadable storage device including instructions; and one or moreprocessors configured to execute the instructions to perform operationscomprising: storing a representation of elements of a physical structurein a computer aided design (CAD) model; providing the representation ofelements to a first analysis program for application of simulated loadsto the representation of elements; storing in the CAD model first loadinformation that specifies the simulated loads applied by the firstanalysis program; providing the representation of elements to a secondanalysis program for application of simulated loads to therepresentation of elements; and storing in the CAD model second loadinformation that specifies the simulated loads applied by the secondanalysis program so that the CAD model includes a history of loadsapplied by the first and second analysis programs.
 38. The system ofclaim 37, wherein the operations further comprise: modifying therepresentation of elements based on result information that identifieschanges to the representation of elements and that was determined by thefirst analysis program's application of the simulated loads to therepresentation of elements; and wherein the representation of elementsthat is provided to the second analysis program has been modified basedon the result information.
 39. The system of claim 38, wherein theoperations further comprise: receiving the result information by a CADtool application program and from the analysis program; and wherein theCAD tool performs the modifying of the representation of elements. 40.The system of claim 39: wherein providing the representation of elementsto the second analysis program includes providing the first loadinformation to the second analysis program; and wherein the operationsfurther comprise extracting, by the second analysis program, the resultinformation that identifies changes to the representation of elementsfrom the CAD model using the first load information provided to thesecond analysis program.
 41. The system of claim 37, wherein providingthe representation of elements to the second analysis program includesproviding the first load information to the second analysis program. 42.The system of claim 37, wherein providing the representation of elementsto the second analysis program includes automatically transferring thefirst load information to the second analysis program without receivinguser input that manually transfers to the second analysis program thesimulated loads that were applied by the first analysis program.
 43. Thesystem of claim 37, wherein the operations further comprise: receivinguser input to create a physical element in a physical representation ofelements that is stored in the CAD model; and in response to receivingthe user input to create the physical element, generating the physicalelement in the physical representation of elements, and generating acorresponding analytical element in the representation of elements thatis stored in the CAD model.
 44. The system of claim 37, wherein thestoring and providing are performed by a CAD tool application programexecuting on a computer system.